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Volumn 52, Issue , 1996, Pages 423-433

Aeroelastic analysis of helicopter rotor blades incorporating anisotropic piezoelectric twist actuation

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; FIBER REINFORCED MATERIALS; PIEZOELECTRIC DEVICES; TURBOMACHINE BLADES;

EID: 0030410693     PISSN: 07334230     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article
Times cited : (10)

References (31)
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  • 9
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    • Giurgiutiu, V.1    Chaudhry, Z.2    Rogers, C.3
  • 11
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    • Ham, N.1
  • 12
    • 85003253286 scopus 로고
    • Torsional Oscillations of Helicopter Blades Due to Stall
    • May-June
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    • Loewy, R.1
  • 18
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    • Using Adaptive Structures to Attenuate Rotary Wing Aeroelastic Response
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  • 19
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    • July
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    • Sept.-Oct.
    • Peters, D. A., Chouchane, M., and Fulton, M., "Helicopter Trim with Flap-Lag-Torsion and Stall by an Optimized Controller," Journal of Guidance, Control and Dynamics, Vol. 13, No. 5, pp. 824-834, Sept.-Oct., 1990.
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    • Tran, C.T.1    Petot, D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.